mirror of https://github.com/ArduPilot/ardupilot
b163e13964
These concern the TAKEOFF flight stage and address #27147. * Logging metadata fixes * Disabled continuous TECS reset during takeoff * Fixed bug in reached_speed_takeoff calculation * Limited SPDWEIGHT=2 to only first part of takeoff climb * _post_TO_hgt_offset set to constant * Takeoff I-gain now defaults to 0 and is used * Use at least TRIM_THROTTLE during the climb * Updated description of TECS_TKOFF_IGAIN with new behaviour * Forced max throttle while below TKOFF_LVL_ALT * Added throttle constraints in no-airspeed mode Additionally, set_min_throttle() has been created, that allows one to set the minimum TECS throttle for the next update_pitch_throttle() loop. Additionally, the throttle limits system has been reworked. TECS will receive external throttle limits from Plane and will always take them into account and respect them. |
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| .. | ||
| AP_FixedWing.h | ||
| AP_MultiCopter.h | ||
| AP_Vehicle.cpp | ||
| AP_Vehicle.h | ||
| AP_Vehicle_Type.h | ||
| AP_Vehicle_config.h | ||
| ModeReason.h | ||
| Parameters.cpp | ||